Introducing steam with quench air into turbine engine combustor

Patent metadata

Field	Value
Publication number	US-2025020078-A1
Application number	US-202418899997-A
Country	US
Kind code	A1
Filing date	Sep 27, 2024
Priority date	Mar 14, 2023
Publication date	Jan 16, 2025
Grant date	—

Abstract

An assembly is provided for a turbine engine. This assembly includes a housing, a combustor and a steam injector. The housing includes an air plenum. The combustor is disposed within the air plenum. The combustor includes a combustor wall and a combustion chamber. The combustor wall is disposed between the combustion chamber and the air plenum. The combustor wall includes a quench aperture that extends through the combustor wall from the air plenum to the combustion chamber. The steam injector projects partially into or through the quench aperture.

First claim

What is claimed is:

1 . An assembly for a turbine engine, comprising:
a housing comprising an air plenum; a combustor disposed within the air plenum, the combustor including a combustor wall and a combustion chamber, the combustor wall disposed between the combustion chamber and the air plenum, and the combustor wall comprising a quench aperture that extends through the combustor wall from the air plenum to the combustion chamber; and a steam injector projecting partially into or through the quench aperture, wherein the steam injector is coaxial with the quench aperture.

2 . The assembly of claim 1 , further comprising:
a steam system comprising the steam injector; the steam system configured to direct steam out of the steam injector into the combustion chamber with air flowing through the quench aperture from the air plenum into the combustion chamber.

3 . The assembly of claim 2 , further comprising a mixer configured to mix the steam with the air.

4 . The assembly of claim 2 , wherein
the steam injector is configured with a single steam outlet; and the steam system is configured to direct the steam out of the steam injector through the single steam outlet.

5 . The assembly of claim 2 , wherein
the steam injector is configured with a plurality of steam outlets; and the steam system is configured to direct the steam out of the steam injector through the plurality of steam outlets.

6 . The assembly of claim 1 , wherein the steam injector projects partially into the quench aperture.

7 . The assembly of claim 1 , wherein the steam injector projects through the quench aperture to or into the combustion chamber.

8 . The assembly of claim 1 , wherein
the combustor wall further comprises a chute; and the chute projects partially into the air plenum and extends circumferentially about an inlet to the quench aperture from the air plenum.

9 . The assembly of claim 8 , wherein the chute comprises a tubular body.

10 . The assembly of claim 8 , wherein the chute comprises an arcuate body.

11 . The assembly of claim 1 , wherein the quench aperture has a longitudinal centerline and an elongated cross-sectional geometry in a reference plane perpendicular to the longitudinal centerline.

12 . The assembly of claim 1 , wherein
the quench aperture extends laterally between an upstream side and a downstream side relative to a flow of combustion products within the combustion chamber; and the steam injector is arranged closer to the upstream side than the downstream side.

13 . The assembly of claim 1 , wherein
the quench aperture extends laterally between an upstream side and a downstream side relative to a flow of combustion products within the combustion chamber; and the steam injector is arranged closer to the downstream side than the upstream side.

14 . The assembly of claim 1 , further comprising a second steam injector projecting partially into or through the quench aperture.

15 . An assembly for a turbine engine, comprising:
a housing comprising an air plenum; a combustor disposed within the air plenum, the combustor including a combustor wall and a combustion chamber, the combustor wall disposed between the combustion chamber and the air plenum, the combustor wall comprising a quench aperture that extends longitudinally along a longitudinal centerline through the combustor wall from the air plenum to the combustion chamber, and the quench aperture having an elongated cross-sectional geometry in a reference plane perpendicular to the longitudinal centerline; and a steam system comprising a steam injector aligned with the longitudinal centerline, the steam system configured to direct steam out of the steam injector into the combustion chamber with air flowing through the quench aperture from the air plenum into the combustion chamber.

16 . The assembly of claim 15 , wherein the steam injector is symmetrically positioned with the quench aperture.

17 . The assembly of claim 15 , wherein the steam injector is coaxial with the longitudinal centerline.

18 . The assembly of claim 15 , wherein the steam injector projects partially into the quench aperture.

19 . The assembly of claim 15 , wherein the steam injector projects through the quench aperture.

20 . An assembly for a turbine engine, comprising:
a housing comprising an air plenum; a combustor disposed within the air plenum, the combustor including a combustor wall and a combustion chamber, the combustor wall disposed between the combustion chamber and the air plenum, and the combustor wall comprising a quench aperture that extends through the combustor wall from the air plenum to the combustion chamber; a steam system comprising a steam injector, the steam system configured to direct steam out of the steam injector into the combustion chamber with air flowing through the quench aperture from the air plenum into the combustion chamber, wherein the steam injector is centered relative to the quench aperture; and a mixer configured to mix the steam with the air, the mixer configured as part of or attached to at least one of the steam injector or the combustor wall.

Assignees

• Rtx Corp

Inventors

• Kramer Stephen K
• Smith Lance L
• Boardman Gregory
• Dai Zhongtao

Classifications

• F05D2270/08

  to produce clean exhaust gases · CPC title

• F05D2240/35

  Combustors or associated equipment · CPC title

• F05D2220/32

  in gas turbines · CPC title

• F02C3/30 Primary

  Adding water, steam or other fluids {for influencing combustion, e.g. to obtain cleaner exhaust gases (F02C7/141, F02C7/30, F01D21/00, F01K21/04, F23D11/10 take precedence)} · CPC title

• F23R2900/00002

  Gas turbine combustors adapted for fuels having low heating value [LHV] · CPC title